GOE 227 (MVA H.37) AIRFOIL (goe227-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: GOE 227 (MVA H.37) AIRFOIL (goe227-il) Reynolds number: 1,000,000 Max Cl/Cd: 134.76 at α=2° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-goe227-il-1000000-n5.txt Download as CSV file: xf-goe227-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: GOE 227 (MVA H.37) AIRFOIL
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 1.000 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-13.500 -0.5649 0.05438 0.05121 -0.1233 0.7982 0.0250
-13.250 -0.6128 0.04075 0.03735 -0.1397 0.7912 0.0250
-13.000 -0.6045 0.03293 0.02930 -0.1545 0.7848 0.0253
-12.750 -0.5778 0.02762 0.02381 -0.1664 0.7793 0.0257
-12.500 -0.5439 0.02377 0.01979 -0.1760 0.7722 0.0261
-12.250 -0.5065 0.02087 0.01668 -0.1842 0.7651 0.0265
-12.000 -0.4723 0.01929 0.01493 -0.1887 0.7561 0.0268
-11.750 -0.4408 0.01836 0.01385 -0.1913 0.7458 0.0270
-11.500 -0.4085 0.01717 0.01250 -0.1945 0.7309 0.0276
-11.250 -0.3776 0.01637 0.01153 -0.1965 0.7070 0.0280
-11.000 -0.3477 0.01580 0.01078 -0.1980 0.6810 0.0285
-10.750 -0.3176 0.01533 0.01017 -0.1993 0.6642 0.0289
-10.500 -0.2873 0.01490 0.00962 -0.2004 0.6531 0.0294
-10.250 -0.2567 0.01447 0.00910 -0.2016 0.6464 0.0299
-10.000 -0.2261 0.01407 0.00859 -0.2026 0.6409 0.0303
-9.500 -0.1647 0.01335 0.00769 -0.2046 0.6329 0.0311
-9.250 -0.1340 0.01302 0.00729 -0.2055 0.6300 0.0314
-9.000 -0.1031 0.01269 0.00688 -0.2064 0.6273 0.0318
-8.750 -0.0721 0.01231 0.00645 -0.2074 0.6247 0.0326
-8.500 -0.0413 0.01202 0.00611 -0.2082 0.6223 0.0333
-8.250 -0.0107 0.01178 0.00581 -0.2090 0.6200 0.0341
-7.750 0.0505 0.01134 0.00528 -0.2103 0.6163 0.0357
-7.500 0.0812 0.01114 0.00503 -0.2110 0.6150 0.0364
-7.250 0.1120 0.01092 0.00477 -0.2117 0.6137 0.0373
-7.000 0.1428 0.01071 0.00454 -0.2124 0.6124 0.0386
-6.750 0.1734 0.01054 0.00435 -0.2130 0.6110 0.0399
-6.500 0.2039 0.01039 0.00416 -0.2136 0.6097 0.0413
-6.250 0.2343 0.01026 0.00400 -0.2141 0.6082 0.0425
-6.000 0.2648 0.01012 0.00383 -0.2147 0.6062 0.0444
-5.750 0.2949 0.01002 0.00371 -0.2152 0.6036 0.0465
-5.500 0.3249 0.00995 0.00360 -0.2156 0.6008 0.0485
-5.250 0.3552 0.00986 0.00348 -0.2161 0.5989 0.0503
-5.000 0.3856 0.00975 0.00338 -0.2167 0.5978 0.0525
-4.750 0.4159 0.00966 0.00329 -0.2171 0.5964 0.0546
-4.500 0.4461 0.00959 0.00319 -0.2176 0.5946 0.0563
-4.250 0.4763 0.00950 0.00309 -0.2181 0.5925 0.0581
-4.000 0.5065 0.00943 0.00302 -0.2185 0.5908 0.0604
-3.750 0.5365 0.00938 0.00296 -0.2189 0.5891 0.0626
-3.500 0.5663 0.00935 0.00291 -0.2193 0.5874 0.0646
-3.250 0.5960 0.00933 0.00286 -0.2196 0.5858 0.0658
-3.000 0.6260 0.00927 0.00279 -0.2201 0.5842 0.0681
-2.750 0.6557 0.00924 0.00275 -0.2205 0.5822 0.0707
-2.500 0.6857 0.00919 0.00271 -0.2209 0.5807 0.0734
-2.250 0.7157 0.00915 0.00267 -0.2213 0.5792 0.0752
-2.000 0.7455 0.00913 0.00264 -0.2216 0.5778 0.0765
-1.750 0.7755 0.00907 0.00259 -0.2221 0.5763 0.0797
-1.500 0.8053 0.00903 0.00256 -0.2225 0.5745 0.0828
-1.250 0.8349 0.00901 0.00254 -0.2228 0.5721 0.0861
-1.000 0.8643 0.00900 0.00253 -0.2231 0.5693 0.0897
-0.750 0.8936 0.00900 0.00253 -0.2234 0.5665 0.0970
-0.500 0.9230 0.00899 0.00254 -0.2238 0.5644 0.1078
-0.250 0.9528 0.00894 0.00255 -0.2242 0.5626 0.1243
0.000 0.9825 0.00890 0.00256 -0.2246 0.5597 0.1395
0.250 1.0119 0.00888 0.00257 -0.2249 0.5559 0.1523
0.500 1.0411 0.00886 0.00258 -0.2253 0.5520 0.1709
0.750 1.0709 0.00874 0.00264 -0.2259 0.5484 0.2597
1.000 1.1001 0.00874 0.00270 -0.2262 0.5452 0.2798
1.250 1.1290 0.00876 0.00276 -0.2264 0.5403 0.2945
1.500 1.1572 0.00882 0.00282 -0.2265 0.5335 0.3046
1.750 1.1855 0.00889 0.00288 -0.2266 0.5252 0.3118
2.000 1.2128 0.00900 0.00295 -0.2265 0.5106 0.3192
2.250 1.2377 0.00928 0.00309 -0.2261 0.4815 0.3250
2.500 1.2605 0.00972 0.00335 -0.2252 0.4500 0.3315
2.750 1.2842 0.01009 0.00363 -0.2246 0.4283 0.3409
3.000 1.3087 0.01041 0.00387 -0.2241 0.4130 0.3482
3.250 1.3335 0.01068 0.00411 -0.2236 0.4017 0.3565
3.500 1.3592 0.01088 0.00430 -0.2233 0.3938 0.3649
3.750 1.3845 0.01111 0.00450 -0.2229 0.3874 0.3712
4.000 1.4107 0.01125 0.00467 -0.2227 0.3823 0.3807
4.250 1.4361 0.01144 0.00488 -0.2224 0.3763 0.3937
4.500 1.4607 0.01166 0.00511 -0.2219 0.3705 0.4100
4.750 1.4866 0.01180 0.00530 -0.2216 0.3668 0.4254
5.250 1.5361 0.01218 0.00574 -0.2208 0.3577 0.4595
5.500 1.5597 0.01241 0.00600 -0.2201 0.3524 0.4797
5.750 1.5839 0.01260 0.00624 -0.2196 0.3470 0.5009
6.000 1.6059 0.01289 0.00654 -0.2186 0.3396 0.5200
6.250 1.6277 0.01318 0.00683 -0.2177 0.3319 0.5364
6.500 1.6484 0.01348 0.00714 -0.2165 0.3246 0.5506
6.750 1.6665 0.01381 0.00747 -0.2148 0.3177 0.5636
7.000 1.6829 0.01417 0.00783 -0.2128 0.3085 0.5762
7.250 1.6995 0.01461 0.00827 -0.2110 0.2984 0.5894
7.500 1.7151 0.01513 0.00877 -0.2091 0.2881 0.6031
7.750 1.7332 0.01554 0.00921 -0.2076 0.2804 0.6198
8.000 1.7477 0.01614 0.00982 -0.2056 0.2699 0.6436
8.250 1.7600 0.01683 0.01066 -0.2034 0.2531 0.7758
8.500 1.7642 0.01760 0.01158 -0.1998 0.2333 1.0000
8.750 1.7695 0.01882 0.01270 -0.1967 0.2137 1.0000
9.000 1.7714 0.02034 0.01409 -0.1932 0.1905 1.0000
9.250 1.7547 0.02320 0.01667 -0.1877 0.1453 1.0000
9.500 1.7509 0.02536 0.01871 -0.1842 0.1217 1.0000
9.750 1.7544 0.02709 0.02039 -0.1816 0.1088 1.0000
10.000 1.7586 0.02882 0.02208 -0.1793 0.0975 1.0000
10.250 1.7467 0.03187 0.02496 -0.1754 0.0658 1.0000
10.500 1.7292 0.03557 0.02853 -0.1714 0.0346 1.0000
10.750 1.7318 0.03765 0.03061 -0.1693 0.0276 1.0000
11.000 1.7373 0.03953 0.03252 -0.1676 0.0240 1.0000
11.250 1.7424 0.04151 0.03452 -0.1660 0.0212 1.0000
11.500 1.7489 0.04340 0.03645 -0.1646 0.0194 1.0000
11.750 1.7542 0.04542 0.03850 -0.1631 0.0178 1.0000
12.000 1.7599 0.04747 0.04059 -0.1618 0.0166 1.0000
12.250 1.7653 0.04959 0.04275 -0.1606 0.0156 1.0000
12.500 1.7702 0.05180 0.04501 -0.1594 0.0148 1.0000
12.750 1.7744 0.05413 0.04737 -0.1582 0.0140 1.0000
13.000 1.7788 0.05644 0.04975 -0.1571 0.0135 1.0000
13.250 1.7831 0.05880 0.05216 -0.1561 0.0131 1.0000
13.500 1.7870 0.06121 0.05463 -0.1550 0.0126 1.0000
13.750 1.7896 0.06382 0.05729 -0.1540 0.0122 1.0000
14.000 1.7917 0.06648 0.06000 -0.1531 0.0117 1.0000
14.250 1.7925 0.06932 0.06289 -0.1521 0.0113 1.0000
14.500 1.7927 0.07223 0.06587 -0.1512 0.0109 1.0000
14.750 1.7947 0.07493 0.06863 -0.1503 0.0107 1.0000
15.000 1.7954 0.07784 0.07161 -0.1495 0.0104 1.0000
15.250 1.7960 0.08076 0.07460 -0.1488 0.0101 1.0000
15.500 1.7952 0.08391 0.07782 -0.1481 0.0098 1.0000
15.750 1.7945 0.08702 0.08098 -0.1475 0.0096 1.0000
16.000 1.7919 0.09043 0.08447 -0.1469 0.0093 1.0000
16.250 1.7902 0.09375 0.08785 -0.1464 0.0091 1.0000
16.500 1.7861 0.09746 0.09164 -0.1460 0.0089 1.0000
16.750 1.7819 0.10122 0.09547 -0.1457 0.0086 1.0000
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